An event-trigger control scheme for spacecraft attitude control

• المؤلف الرئيسي: Leong, Wei Yang
• مؤلفون آخرون: Wen Changyun
• التنسيق: Final Year Project
• اللغة: English
• منشور في: 2017
• الموضوعات: DRNTU::Engineering::Electrical and electronic engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/71837
• المؤسسة: Nanyang Technological University

This report discussed on the proposal of event-trigger control design scheme for spacecraft attitude stabilization problem to reduce communication burden between spacecraft attitude controller and actuator. Both controller and event-trigger controller are designed simultaneously in order to compensa...